| 摘要 |
The invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connected to a central liquid cooling system of an aircraft in order to feed a liquid coolant medium at a desired low temperature to the liquid cooling device, and wherein the coolant line (16) of the liquid cooling device is in thermal surface contact with the modular signal computer units (12) in order to dissipate heat from the modular signal computer units (12).
|
